L1011-200F full freighter aircraft with
higher volumetric capacity (470-488 cbm), a little less payload 56 Ton and
a little less range (6BH at full payload) than a DC10-30F.
MSN 1198
Aircraft Specifications:
L1011-200F
S/N 293C-1198
REGISTRATION
SX-CVE
SERIAL NUMBER
293C-1198
MAKE AND MODEL
LOCKHEED L1011-385-1-15
DESIGNATION
L1011-200F
DATE OF BUILD
DECEMBER 1980
ORIGINAL OPERATOR
BRITISH AIRWAYS
ENGINE TYPE
ROLLS ROYCE RB211-524B2
FUEL QUANTITY
178,000 LBS/81,000 KGS
CONFIGURATION
CARGO
AIRCRAFT TOTAL HOURS
46,462 HOURS
AIRCRAFT TOTAL CYCLES
12,440 CYCLES
CURRENT CYCLE RATIO
3.73 HOURS/CYCLE
LAST SERVICE FLIGHT
NOVEMBER 2004
NOISE COMPLIANCE
STAGE III
DATE OF DATA
SEPTEMBER 2006
WEIGHTS
M.T.O.W.
474,000 LBS /215,000
KGS
M.Z.F.W.
350,000 LBS /
158,000 KGS
M.L.W.
368,000 LBS/
167,000KGS
O.E.W.
222,610 LBS /
100,974 KGS
FUEL CAPACITY
178,400 LBS / 81,000
KGS
PAYLOAD
Approx 123,500 LBS
/56,000 KGS
CUBIC LOAD
470 CBM (or 488 CBM
with LD3’s in C1 hold)
MAINTENANCE INTERVALS AND
REMAINING POTENTIALS
A CHECK PERIOD
350 Hours
C CHECK PERIOD
4,200 HOURS
NEXT C CHECK
50,662 HOURS T.T.
C CHECK TIME TO GO
4,200 HOURS
ENGINES
POSITION
1
2
3
SERIAL No.
14510
14545
14507
DATA AS AT
:
Sep 2006
Sep 2006
Sep 2006
TOTAL HOURS
36,100
42,958
43,454
TOTAL
CYCLES
9,103
11,073
11,511
C.S.L.S.V.
1,239
2
708
FIRST
LIMITER
HCPT shaft
IPC-6-7
HPC-1
CYCLES
REMAIN
2,396
2,379
3,160
LANDING GEAR
POSITION
NOSE
LEFT
RIGHT
SERIAL No.
BOA18739
BOA19274
M0046
DATE DUE
Mar 2009
Nov 2008
Nov 2008
CYCLES REM.
9,428
9,257
9,257
Note: Landing gear overhaul
life is 10 year or 10,000 cycles whichever occurs first
APU
MAKE
HAMILTON STANDARD
MODEL
ST6L-73
SERIAL NUMBER
55329
DATA AS AT
September 2006
TOTAL HOURS /
CYCLES
17,344 / 17,900
FIRST LIMITER
Power Turbine Disc
CYCLES REMAINING
4,419
TIME CALCULATION
1.5 APU hours and
2 APU cycles per Aircraft Cycle
CONFIGURATION
LAYOUT
CARGO
UPPER DECK
23 Pallets - 88 inch x 125 inch
ALTERNATE UPPER
DECK
22 Pallets – 96 inch x 125 inch
Plus 1 Pallet – 88 inch x 125 inch
ALTERNATE UPPER
DECK
26 Pallets 88 inch x 108 inch
C1 HOLD
5 Pallets 88 inch x 125 inch
Or Misc. LD3 and/or LD6
C2 HOLD
Misc. LD3 and/or LD6
C3 HOLD
Bulk Loading
COURIER AREA
2 DOUBLE BUSINESS
CLASS SEATS
3 BUNK BEDS
SELF CONTAINED
TOILET
GALLEY UNIT
GALLEY UNIT
MICROWAVE OVEN
COFFEE MAKER
MISC. CUPBOARDS
AVIONICS
UNIT
E&E Bay
Location
MANUF.
MODEL
PART NUMBER
GPS
Cockpit
Trimble
2101
I/O
Weather Radar #1
Front
Rack 1
RCA
AVQ30X
MI-592041-2
Weather Radar #2
Front
Rack 1
RCA
AVQ30X
MI-592041-2
Instrument Monitor Comparitor
Front
Rack 1
Sperry
2583723-903
INS #1
Front
Rack 2
Delco
Carousel
7890860-011
INS #2
Front
Rack 2
Delco
Carousel
7890860-011
INS #3
Front
Rack 2
Delco
Carousel
7890860-011
INS
Battery #1
Front
LHS
INS
Battery #2
Front
LHS
INS
Battery #3
Front
LHS
Flight
Station Temp. Controller
RHS 1
Ham.
Std.
ED724406-2
Courier Zone Temp. Controller
RHS 1
Ham.
Std.
ED724406-2
Fwd
Cabin Temp. Controller
RHS 1
Ham.
Std.
ED724406-2
#1
Pack Controller
RHS 1
Ham.
Std.
763880-1
ECS
System Test
RHS 1
Ham.
Std.
763870-1
Essential Transformer/Rectifier
RHS 1
Lynwood
2-418-03
ECS
Pressure Controller
RHS 2
Ham.
Std.
ED724436-5
#2
Pack Controller
RHS 2
Ham.
Std.
763880-1
#3
Pack Controller
RHS 2
Ham.
Std.
763880-1
Aft
Cabin Temp. Controller
RHS 2
Ham.
Std.
ED724406-2
FCES
Computer
LHS
Fwd 1
Collins
562T-1
787-6027-001
AFCS
Trim Aug Computer
LHS
Fwd 1
Collins
562T-2
787-6639-005
Speed
Control Computer
LHS
Fwd 1
Collins
562S-3
787-6024-008
Landing Gear Logic Box
LHS
Fwd 1
Lockheed
1519207-115
AFCS
Pitch Computer #2
LHS
Fwd 2
Collins
562P-4
787-6022-011
SAS
Yaw Computer #2
LHS
Fwd 2
Collins
562Y-4
787-6025-002
AFCS
Roll Computer #2
LHS
Fwd 2
Collins
562R-4
787-6023-005
AFCS
Pitch Computer #1
LHS
Fwd 3
Collins
562P-4
787-6022-011
SAS
Yaw Computer #1
LHS
Fwd 3
Collins
562Y-4
787-6025-002
AFCS
Roll Computer # 1
LHS
Fwd 3
Collins
562R-4
787-6023-005
Load
Limiter Computer
LHS
Fwd 3
Lockheed
56413-005
Flight
Control Aux. Unit
LHS
Fwd 4
Lockheed
25-1560306-103
HF
Transceiver #1
LHS
Aft 1
Collins
618T
522-4829-001
HF
Transceiver #2
LHS
Aft 1
Collins
618T
522-1501-000
Air
Data Computer #1
LHS
Aft 1
Sperry
4031800-902
Air
Data Computer #2
LHS
Aft 1
Sperry
4031800-902
Flight Mgmt Computer
LHS
Aft 2
Ham.
Std.
2-00063-801-11
Inertial Accessory. Unit
LHS
Aft 2
Lockheed
25-161953-119
Selcal
LHS
Aft 2
Motorola
NA135
DME #1
LHS
Aft 3
Collins
860E-3
522-4209-001
DME #2
LHS
Aft 3
Collins
860E-3
522-4209-001
Galley
Power Inverter
LHS
Aft 3
SPH-1606B-3
ILS
#1
LHS
Aft 4
Collins
ILS70
792-6021-002
ILS #2
LHS
Aft 4
Collins
ILS70
792-6021-002
VHF
Accessory Unit
LHS
Aft 4
Lockheed
1556893-115
VOR #1
LHS
Aft 4
Collins
51R-6
822-0761-001
VOR #2
LHS
Aft 4
Collins
51R-6
822-0847-001
GPWS
LHS
Aft 4
Sunstrand
Mk VII
965-0876-001-B03-B04
VHF
Com #1
LHS
Aft 4
Collins
618M
622-1181-003
VHF
Com #2
LHS
Aft 4
Collins
618M
ATC #1
LHS
Aft 5
Honeywell
TCAS
II
066-50000-2120
ATC #2
LHS
Aft 5
Honeywell
Mode C
066-01127-1301
PA
Amplifier
LHS
Aft 5
Pacific Electronics
255-5
Service Interphone Amp.
LHS
Aft 5
Telephonics
409E700
Flight
Interphone Amp.
LHS
Aft 5
Telephonics
409E700
Audio
Distribution Unit
LHS
Aft 5
Lockheed
1555744/1
Marker
Beacon
LHS
Aft 5
Collins
51Z-4
522-2996-018
Heading Coupler Accy Unit
LHS
Aft 5
Lockheed
25156695310
Magnetic Heading Compass Coupler
LHS
Aft 5
Sperry
2591201-903
Magnetic Heading Compass Coupler
LHS
Aft 5
Honeywell
2591201-903
FDAU
LHS
Mid
Teledyne
70-201T
2222601-45
ELT
Cockpit
Narco
607690-2
Complies with European
ACAS 7 (TCAS II), RVSM and 8.33 spacing requirements
The above aircraft data
are given for information purposes only, without any responsibility for the
Seller/Lessor, and need to be verified by the Purchaser or Lessee of the
aircraft as to their accuracy.
Specification and photos are not contractual and
are subject to verification upon inspection
NB:
Aircraft offered for sale subject to contract, prior sale, withdrawal from
the market and information regarding any aircraft or helicopter and provided
verbally or in written documentation and/or contained within this e.mail or
associated paper-work should be taken as a guide only in determining the
suitability, including that aircraft or helicopters specification and/or
performance. We highly recommend that any buyer or lessee perform their own
inspections and due diligence to verify any and all technical, perfomance
and specification information contained therein including OEM claims.
TAKE NOTICE!
PLEASE BE ADVISED THAT INFORMATION INCLUDED IS CONFIDENTIAL IN NATURE AND IS
BASED ON PREXISTING BUSINESS RELATIONSHIP WITH THE LEGAL OWNER OF PROPERTY
DESCRIBED HEREIN (IF APPLICABLE). AS SUCH, UPON RECEIPT OF SAID INFORMATION
THE RECEIVER AKNOWLEDGES THAT ANY UNAUTHORIZED CONTACT WITH SAID LEGAL
SELLER WILL BE CHARACTERIZED AS A BREACH OF CONFIDENTIALITY AND SAID
AGREEMENT MAY BE ENFORCED UNDER EXISTING LAW OR IN EQUITY.
This paper was prepared by
General Equipment Corp.
The paper represents an offer of a partner of General Equipment Corp.
All rights are reserved by and for General Equipment Corp.. All
content and ideas of this paper are the property of General Equipment Corp.
